WO2015190169A1 - 回転機械及び回転機械の組立方法、回転機械のメンテナンス方法 - Google Patents

回転機械及び回転機械の組立方法、回転機械のメンテナンス方法 Download PDF

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Publication number
WO2015190169A1
WO2015190169A1 PCT/JP2015/061163 JP2015061163W WO2015190169A1 WO 2015190169 A1 WO2015190169 A1 WO 2015190169A1 JP 2015061163 W JP2015061163 W JP 2015061163W WO 2015190169 A1 WO2015190169 A1 WO 2015190169A1
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WO
WIPO (PCT)
Prior art keywords
casing
support pad
rotating machine
combustor
intermediate shaft
Prior art date
Application number
PCT/JP2015/061163
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
橋本　真也
拓郎 亀田
Original Assignee
三菱日立パワーシステムズ株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 三菱日立パワーシステムズ株式会社 filed Critical 三菱日立パワーシステムズ株式会社
Priority to KR1020167032646A priority Critical patent/KR101874732B1/ko
Priority to US15/313,392 priority patent/US10174676B2/en
Priority to DE112015002713.0T priority patent/DE112015002713B4/de
Priority to CN201580027305.4A priority patent/CN106460561B/zh
Publication of WO2015190169A1 publication Critical patent/WO2015190169A1/ja

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/72—Maintenance
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/31—Retaining bolts or nuts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00019—Repairing or maintaining combustion chamber liners or subparts

Definitions

  • the present invention relates to a rotating machine such as a gas turbine or a steam turbine, a rotating machine assembly method, and a rotating machine maintenance method.
  • a general gas turbine is composed of a compressor, a combustor, and a turbine.
  • the compressor compresses the air taken in from the air intake port into high-temperature and high-pressure compressed air.
  • the combustor obtains high-temperature and high-pressure combustion gas by supplying fuel to the compressed air and burning it.
  • the turbine is driven by this combustion gas, and drives a generator connected on the same axis.
  • the combustor is supported by an intermediate shaft cover, and the intermediate shaft cover has an outer peripheral end fitted into a fitting portion of the upper casing and fixed by a bolt. Therefore, when the worker maintains the combustor, the intermediate shaft cover and the upper casing are separated by loosening and removing the bolts, and the upper casing is removed to expose the combustor.
  • Patent Document 1 An example of such a gas turbine is described in Patent Document 1 below.
  • the outer peripheral end of the intermediate shaft cover that supports the combustor is fitted to the fitting portion of the upper casing and is fixed by bolts.
  • the upper casing is removed by loosening the bolt.
  • the bolt fastening part between the intermediate shaft cover and the upper casing becomes high temperature during the operation of the gas turbine, and the screw part of the bolt is seized, making it difficult to loosen the bolt, which hinders the maintenance of the combustor. There is a problem of end.
  • the present invention solves the above-described problems, and an object thereof is to provide a rotating machine, a rotating machine assembly method, and a rotating machine maintenance method that facilitate the removal of a casing and improve internal maintenance. .
  • a rotating machine is a rotating machine in which a rotating body is rotatably supported in a casing, and an outer casing composed of upper and lower outer casing portions having a half crack shape, An inner casing that is composed of upper and lower inner casing portions having a cracked shape and is installed inside the outer casing, and a radial fitting portion between the outer casing and the inner casing is pressed in the axial direction of the rotating body And a pressing support mechanism for supporting.
  • the outer casing can be removed from the inner casing simply by releasing the pressing between the outer casing and the inner casing by the pressing support mechanism. Further, even if the pressing between the outer casing and the inner casing by the pressing support mechanism cannot be released, the pressing between the outer casing and the inner casing is not released by applying a load to the outer casing in the radial direction. Even the outer casing can be removed. As a result, it is possible to easily remove the casing and improve the maintainability of the internal structure.
  • the pressing support mechanism has a support pad that is screw-engaged with one of the fitting portion of the outer casing and the fitting portion of the inner casing and presses against the other.
  • the support pad can be used to support and release the pressing of the outer casing and the inner casing, and the workability of the assembling work and the dismantling work in the outer casing can be improved.
  • the fitting portion of the outer casing has a concave shape
  • the fitting portion of the inner casing has a convex shape
  • the support pad is screw-engaged with the fitting portion of the inner casing. It is characterized by that.
  • the rotating machine according to the present invention is characterized in that a detent mechanism for preventing rotation of the support pad is provided.
  • the rotation preventing mechanism includes a locking member that locks to a base end portion of the support pad, and a fixing member that fixes the locking member to the outer casing or the inner casing. It is characterized by.
  • the locking member is locked to the base end portion of the support pad, and the locking member is fixed to the outer casing or the inner casing by the fixing member. Therefore, the rotation of the support pad can be easily prevented with a simple configuration, and when the fixing member is seized, the locking member can be removed by removing the fixing member.
  • the rotary machine of the present invention is characterized in that a centering mechanism for supporting the inner casing so as to be movable in the radial direction with respect to the outer casing is provided.
  • the inner casing is movable in the radial direction with respect to the outer casing by the centering mechanism, the centers of the casings are not shifted even if the outer casing and the inner casing are heated.
  • the rotary shaft is rotatably supported through a bearing in a casing that is half-cracked in the vertical direction, and inside the casing and on the outer peripheral side of the rotary shaft.
  • the step of fitting the upper casing in the casing with the end portion of the inner casing in the radial direction, and the fitting portion between the casing and the inner casing by the support pad And a step of pressing and supporting in the axial direction.
  • the upper casing and the inner casing are pressed and supported by the support pad in the axial direction, the upper casing can be removed from the inner casing simply by releasing the pressing of the upper casing and the inner casing by the support pad. it can. Further, even if the pressing of the upper casing and the inner casing by the support pad cannot be released, the upper casing and the inner casing are released by pressing the upper casing and the inner casing by releasing the load in the radial direction. The casing can be removed. As a result, it is possible to easily remove the casing and improve the maintainability of the combustor.
  • the support pad is threadedly engaged with one of the upper casing and the inner casing, and when the upper casing is fitted to an end of the inner casing, the support pad is supported. The pad is rotated to press against the other of the upper casing and the inner casing.
  • the upper casing and the inner casing can be pressed and released by the support pad, and the workability of the assembling work and the dismantling work in the upper casing can be improved.
  • the support pad is prevented from rotating with respect to the upper casing and the intermediate shaft cover. It is said.
  • a rotary shaft is rotatably supported via a bearing in a casing having a half-crack shape in the vertical direction, and the inside of the casing and on the outer peripheral side of the rotary shaft.
  • a step of releasing the fastening between the upper casing and the lower casing in the casing, a step of lifting and removing the upper casing from the lower casing, and maintaining the inside of the casing A step, a step of radially fitting the upper casing to an end portion of the inner casing, and a support pad pressing and supporting the fitting portion of the upper casing and the inner casing in the axial direction of the rotating shaft.
  • a step of fastening the upper casing to the lower casing is fastening the upper casing to the lower casing. That.
  • the upper casing and the inner casing are pressed and supported by the support pad in the axial direction, the upper casing can be removed from the inner casing simply by releasing the pressing of the upper casing and the inner casing by the support pad. it can. Further, even if the pressing of the upper casing and the inner casing by the support pad cannot be released, the upper casing and the inner casing are released by pressing the upper casing and the inner casing by releasing the load in the radial direction. The casing can be removed. As a result, it is possible to easily remove the casing and improve the maintainability of the combustor.
  • the upper casing and the inner casing are pressed and supported in the axial direction by the pressing support mechanism (support pad).
  • the maintainability of the internal structure (combustor) can be improved.
  • FIG. 1 is a cross-sectional view showing the vicinity of a combustor in the gas turbine of the present embodiment.
  • FIG. 2 is a front view showing the intermediate shaft cover.
  • FIG. 3 is a front view showing an attachment portion of the intermediate shaft cover by the fixed pad.
  • 4 is a cross-sectional view taken along the line IV-IV in FIG. 5 is a cross-sectional view taken along the line VV of FIG. 6 is a cross-sectional view taken along the line VI-VI in FIG.
  • FIG. 7 is a front view showing an attaching portion of the intermediate shaft cover by the centering pin.
  • FIG. 8 is a cross-sectional view taken along the line VIII-VIII of FIG. 7 showing the attachment portion of the intermediate shaft cover by the centering pin.
  • FIG. 9 is a cross-sectional view taken along the line IX-IX in FIG. 7 showing a mounting portion of the intermediate shaft cover by the centering pin.
  • 10 is a cross-sectional view taken along the line XX of FIG.
  • FIG. 11 is a flowchart showing a work procedure of the maintenance method of the combustor.
  • FIG. 12 is a schematic diagram illustrating a method of fixing the intermediate shaft cover with a fixing pad.
  • FIG. 13 is a schematic diagram illustrating a method of fixing the intermediate shaft cover with a fixing pad.
  • FIG. 14 is a schematic diagram illustrating the overall configuration of the gas turbine.
  • FIG. 14 is a schematic diagram showing the overall configuration of the gas turbine of the present embodiment.
  • the gas turbine of this embodiment is comprised by the compressor 11, the combustor 12, and the turbine 13, as shown in FIG.
  • the compressor 11 and the turbine 13 are arranged along the direction of the axis O outside the rotating shaft 32, and a plurality of combustors 12 are arranged between the compressor 11 and the turbine 13. Yes.
  • the gas turbine is connected to a generator (motor) (not shown) on the same axis, and can generate power.
  • the compressor 11 has an air intake 20 for taking in air, an inlet guide vane (IGV: Inlet Guide Vane) 22 is disposed in the compressor casing 21, and a plurality of stationary blades 23 and a plurality of moving blades. 24 are alternately arranged in the air flow direction (the direction of the axis O of the rotor 32 to be described later), and an extraction chamber 25 is provided on the outside thereof.
  • the compressor 11 generates high-temperature and high-pressure compressed air by compressing the air taken in from the air intake port 20 and supplies the compressed air to the casing 14.
  • the compressor 11 is started by an electric motor connected on the same axis.
  • the combustor 12 is supplied with high-temperature and high-pressure compressed air and fuel that are compressed by the compressor 11 and stored in the casing 14, and burns to generate combustion gas.
  • a plurality of stationary blades 27 and a plurality of moving blades 28 are alternately arranged in a turbine casing 26 in the flow direction of combustion gas (the direction of the axis O of the rotor 32).
  • the turbine casing 26 is provided with an exhaust chamber 30 via an exhaust casing 29 on the downstream side.
  • the exhaust chamber 30 has an exhaust diffuser 31 connected to the turbine 13.
  • the turbine 13 is driven by the combustion gas from the combustor 12 and drives a generator connected on the same axis.
  • a rotor (rotary shaft) 32 is disposed along the direction of the axis O so as to penetrate the central portion of the exhaust chamber 30.
  • the end of the rotor 32 on the compressor 11 side is rotatably supported by the bearing portion 33, and the end of the exhaust chamber 30 side is rotatably supported by the bearing portion 34.
  • the rotor 32 is fixed by a compressor 11 in which a plurality of disks on which the moving blades 24 are mounted are stacked.
  • a plurality of disks on which the moving blades 28 are mounted are fixed in a stack in the turbine 13, and a drive shaft of a generator is connected to an end on the air intake 20 side.
  • the compressor casing 21 of the compressor 11 is supported by the legs 35
  • the turbine casing 26 of the turbine 13 is supported by the legs 36
  • the exhaust chamber 30 is supported by the legs 37.
  • the air taken in from the air intake 20 passes through the inlet guide vane 22, the plurality of stationary vanes 23, and the moving blades 24, and is compressed into high-temperature and high-pressure compressed air.
  • a predetermined fuel is supplied to the compressed air in the combustor 12 and burned.
  • the high-temperature and high-pressure combustion gas generated in the combustor 12 drives and rotates the rotor 32 by passing through the plurality of stationary blades 27 and the moving blades 28 in the turbine 13, and is connected to the rotor 32. Drive the generator. And the combustion gas which drove the turbine 13 is discharge
  • a plurality of combustors 12 are arranged at predetermined intervals in the circumferential direction between the compressor 11 and the turbine 13.
  • Each combustor 12 is supported outside the intermediate shaft cover, and the outer peripheral end of the intermediate shaft cover is connected to the combustor casing. Therefore, when maintaining the combustor, after releasing the fastening of the combustor casing and releasing the connection with the intermediate shaft cover, the combustor casing is removed and maintenance work of the combustor is performed.
  • FIG. 1 is a cross-sectional view showing the vicinity of a combustor in the gas turbine of the present embodiment
  • FIG. 2 is a front view showing an intermediate shaft cover
  • FIG. 3 is a front view showing an attachment portion of the intermediate shaft cover by a fixed pad
  • 4 is a cross-sectional view taken along the line IV-IV in FIG. 3 showing the attachment portion of the intermediate shaft cover by the fixing pad
  • FIG. 5 is a cross-sectional view taken along the line VV in FIG. 4, and FIG. is there.
  • the combustor casing (outer casing) 41 has a cylindrical shape along the direction of the axis O of the rotor 32 (see FIG. 14).
  • This combustor casing 41 is composed of an upper casing (outer casing part) 42 and a lower casing (outer casing part) 43 having a half-crack shape, and a plurality of left and right outer peripheral flange parts 42a, 43a are in close contact with each other.
  • the bolts 44 are integrally connected.
  • the upper casing 42 has a notch portion 42b formed in the outer peripheral flange portion 42a, and a jack (elevating device) 45 can be disposed.
  • the combustor casing 41 has a mounting flange 41a formed on one side in the direction of the axis O, and a mounting flange 41b formed on the other side.
  • the mounting flange 41 a is in close contact with the mounting flange 21 a of the compressor casing (casing) 21 and is connected by a bolt 46
  • the mounting flange 41 b is in close contact with the mounting flange 26 a of the turbine casing (casing) 26.
  • the bolts 47 are connected.
  • the combustor casing 41 is provided with a plurality of combustors 12 at predetermined intervals in the circumferential direction.
  • the combustor outer cylinder 51 is disposed in an attachment hole formed in the combustor casing 41, and a combustor inner cylinder 52 is supported at a predetermined interval inside, and the combustor inner cylinder 52 is disposed at a tip portion.
  • a combustor tail cylinder 53 is connected.
  • a pilot combustion burner 54 is arranged at the center of the inside, and a plurality of main combustion burners 55 are arranged on the inner peripheral surface so as to surround the pilot combustion burner 54 along the circumferential direction.
  • the tip of the combustor tail cylinder 53 is connected to the turbine stationary blade 27.
  • the combustor outer cylinder 51 is fitted with a top hat portion 56 and fastened by a plurality of fastening bolts (not shown), and fuel ports 57, 58, 59 are provided in the top hat portion 56.
  • a pilot fuel line (not shown) is connected to the fuel port 57 of the pilot combustion burner 54
  • a main combustion line (not shown) is connected to the fuel port 58 of each main combustion burner 55
  • a top hat combustion line (not shown) is connected to the fuel port 59. It is connected.
  • an air flow of high-temperature and high-pressure compressed air flows into the combustor inner cylinder 52, and in this combustor inner cylinder 52, this compressed air is mixed with the fuel injected from the main combustion burner 55 and premixed. It turns into a swirling flow of air and flows into the combustor tail cylinder 53.
  • the compressed air is mixed with fuel injected from the pilot combustion burner 54, burned as a seed fire (not shown), and burned as a combustion gas into the combustor tail cylinder 53.
  • the plurality of combustors 12 are supported by an intermediate shaft cover (inner casing) 61.
  • the intermediate shaft cover 61 is disposed in the combustor casing 41 and has a cylindrical shape along the direction of the axis O.
  • the intermediate shaft cover 61 is composed of an upper casing (inner casing portion) 62 and a lower casing (inner casing portion) 63 having a half-crack shape, and a plurality of left and right outer peripheral flange portions 62a, 63a are in close contact with each other.
  • the bolts 64 are integrally connected.
  • the intermediate shaft cover 61 is connected by a plurality of struts 61c having one end 61a and the other end 61b arranged at predetermined intervals in the circumferential direction, and the one end 61a in the direction of the axis O extends to the compressor 11 side.
  • the other end portion 61 b extends to the turbine 13 side and supports the stationary blade 27.
  • the intermediate shaft cover 61 has a cooling manifold 61d, and the cooling air supplied to the cooling manifold 61d is supplied into each stationary blade 27 through a cooling passage (not shown).
  • the intermediate shaft cover 61 has a mounting bracket 65 extending outward from the one end portion 61a.
  • the combustor 12 has the combustor inner cylinder 52 supported by the intermediate shaft cover 61 via the mounting bracket 65. ing.
  • the one end portion 61 a of the combustor casing 41 and the intermediate shaft cover 61 is fitted in the radial direction, and the fitting portion is pressed and supported in the direction of the axis O by the pressing support mechanism 71. Further, the combustor casing 41 and the one end portion 61 a of the intermediate shaft cover 61 are supported by a centering mechanism 72 so as to be movable in the radial direction. A plurality of the pressing support mechanisms 71 and the centering mechanisms 72 are provided at predetermined positions in the circumferential direction at substantially the same position in the radial direction in the combustor casing 41 and the intermediate shaft cover 61.
  • the combustor casing 41 (upper casing 42) is positioned closer to the axis O side than the mounting position of the combustor 12 and has a concave shape.
  • an attachment portion 82 having a ring shape is formed.
  • a fitting portion 83 having a convex shape is formed at one end portion 61a, and a step portion 83a is formed at the fitting portion 83.
  • the recessed fitting portion 81 opens to the axial center O side in the radial direction, and the convex fitting portion 83 faces outward in the radial direction.
  • the fitting portion 83 of the intermediate shaft cover 61 can be fitted to the fitted portion 81 in the combustor casing 41 with a predetermined gap S.
  • the combustor casing 41 is composed of an upper casing 42 and a lower casing 43
  • the intermediate shaft cover 61 is composed of an upper casing 62 and a lower casing 63.
  • the casing 43, the lower casing 63, the upper casing 62, and the upper casing 42 are formed.
  • a through hole 84 is formed in the mounting portion 82 along the direction of the axis O.
  • the intermediate shaft cover 61 has a screw hole 85 and a recess 86 formed in the fitting portion 83.
  • the screw hole 85 is formed on the mounting portion 82 side
  • the concave portion 86 is formed on the side opposite to the mounting portion 82, and the inner diameter of the concave portion 86 is set larger than the inner diameter of the screw hole 85.
  • the support pad 87 has a screw portion 87a and a pressing portion 87b, the screw portion 87a is formed on the base end side (right side in FIG. 4), and is pressed on the distal end side (left side in FIG. 4). A portion 87b is formed. In this case, the outer diameter of the pressing portion 87b is set larger than the outer diameter of the screw portion 87a.
  • the support pad 87 can be screwed into the screw hole 85 of the fitting portion 83 in the intermediate shaft cover 61 at the screw portion 87a, and the pressing portion 87b can enter the concave portion 86 of the fitting portion 83 in the intermediate shaft cover 61. ing.
  • the support pad 87 has a screw portion 87a screwed into the screw hole 85 from the concave portion 86 side.
  • the support pad 87 has a locking hole 87c formed at the base end.
  • the locking hole 87c is a hexagonal hole and is set to a predetermined depth.
  • locking part T1 which makes the hexagonal shape in the tool (for example, torque wrench) T (refer FIG. 13) can latch to the latching hole 87c.
  • the support pad 87 is rotated by rotating the tool T, the support pad 87 can be moved along the axial direction of the screw hole 85.
  • the threaded portion 87 a of the support pad 87 is screwed into the threaded hole 85 of the intermediate shaft cover 61 and the pressing portion 87 b enters the recess 86, so that the intermediate shaft cover 61 is fitted to the fitted portion 81 of the combustor casing 41.
  • the fitting part 83 is fitted, and the attachment part 82 is positioned by contacting the step part 83a.
  • the locking portion T1 of the tool T is locked from the through hole 84 to the locking hole 87c and the support pad 87 is rotated forward by the tool T, the support pad 87 advances along the axial direction of the screw hole 85.
  • the pressing portion 87 b presses against the fitted portion 81 of the combustor casing 41 and the fitting portion 83 presses against the attachment portion 82, so that the combustor casing 41 is pressed and supported by the intermediate shaft cover 61.
  • the support pad 87 is reversely rotated by the tool T, the support pad 87 is retracted along the axial direction of the screw hole 85, and the pressing portion 87 b is separated from the fitted portion 81 in the combustor casing 41 and fitted.
  • the joint portion 83 is separated from the attachment portion 82, the pressure support between the combustor casing 41 and the intermediate shaft cover 61 is released.
  • the pressing support mechanism 71 is provided with a detent mechanism 73 that prevents the support pad 87 from rotating.
  • the anti-rotation mechanism 73 is fixed to a locking rod 91 as a locking member that locks to the base end portion of the support pad 87, and a fixing plate 92 as a fixing member that fixes the locking rod 91 to the combustor casing 41.
  • a bolt 93 and a nut 94 are provided.
  • the locking rod 91 has a threaded portion 91a formed at the base end portion, a flange portion 91b having a ring shape at an intermediate portion, and a locking portion 91c having a hexagonal shape at a distal end portion.
  • the flange portion 91 b can be fitted into the through hole 84 of the attachment portion 81 in the combustor casing 41, and the locking portion 91 c can be locked to the locking hole 87 c of the support pad 87.
  • the fixing plate 92 is formed with a first through hole 92a and a second through hole 92b, and the threaded portion 91a of the locking rod 91 can pass through the first through hole 92a.
  • the fixing bolt 93 can pass through the second through hole 92 b of the fixing plate 92, and the screw portion 93 a can be screwed into the screw hole 82 a formed in the attachment portion 82 of the combustor casing 41.
  • the nut 94 can be screwed into the threaded portion 91 a of the locking rod 91 that passes through the second through hole 92 b of the fixing plate 92.
  • the support pad 87 presses against the fitted portion 81 of the combustor casing 41, the fitting portion 83 presses against the attachment portion 82, and the combustor casing 41 presses against the intermediate shaft cover 61.
  • the support pad 87 is prevented from rotating.
  • the locking portion 91 c of the locking rod 91 is locked from the through hole 84 to the locking hole 87 c of the support pad 87, and the flange portion 91 b is fitted into the through hole 84.
  • the threaded portion 91 a of the locking rod 91 is in close contact with the mounting portion 82 of the combustor casing 41 so that the threaded portion 91 a penetrates the first through hole 92 a of the stationary plate 92, and the threaded portion 93 a of the stationary bolt 93 is connected to the 2 Threaded through the through-hole 92 b to the screw hole 82 a of the mounting portion 82, and the nut 94 can be screwed into the threaded portion 91 a of the locking rod 91.
  • the locking rod 91 is fixed to the combustor casing 41 so that its rotation is restricted, and the rotation of the support pad 87 on which the locking rod 91 is hooked is also restricted.
  • FIG. 7 is a front view showing a mounting portion of the intermediate shaft cover by the centering pin
  • FIG. 8 is a sectional view taken along the line VIII-VIII in FIG. 7 showing the mounting portion of the intermediate shaft cover by the centering pin
  • FIG. 10 is a cross-sectional view taken along the line IX-IX in FIG. 7 and represents a cross-sectional view taken along the line XX in FIG.
  • the combustor casing 41 has a through hole 101 formed in the mounting portion 82 along the direction of the axis O and a circumferential direction in the through hole 101. Screw holes 102 are respectively formed on both sides.
  • the intermediate shaft cover 61 has an engagement groove 103 formed in the fitting portion 83.
  • the through hole 101 of the attachment portion 82 is a circular hole, but the engagement groove 103 of the fitting portion 83 is a groove that is narrower than the inner diameter of the through hole 101, and is on the outer peripheral side of the fitting portion 83. It is open.
  • the centering pin 104 has a cylindrical portion 104a and a guide portion 104b.
  • the cylindrical portion 104a is formed on the proximal end side (upper side in FIG. 8), and the distal end side (lower side in FIG. 8).
  • a guide portion 104b is formed on the top.
  • the outer diameter of the cylindrical portion 104a and the maximum outer diameter of the guide portion 104b are the same, but the width of the guide portion 104b is set small by forming the flat surfaces 104c parallel to each other on the outer peripheral surface. Has been.
  • the centering pin 104 has a cylindrical portion 104 a that can be fitted into the through hole 101 of the mounting portion 82, and a guide portion 104 b that can be engaged with the engaging groove 103 of the fitting portion 83.
  • the flat surface 104c contacts both surfaces of the engaging groove 103.
  • FIG. The centering pin 104 is formed with a screw hole 104d at the base end, and a tool (not shown) is screwed into the screw hole 104d so that the centering pin 104 is engaged with the through-hole 101 and the engagement tool via the tool. It can be extracted from the joint groove 103.
  • the fixing plate 105 has two through holes 105a.
  • each through hole 105a of the fixing plate 105 and each screw hole 102 in the mounting portion are positioned concentrically.
  • the two fixing bolts 106 can pass through the through holes 105 a of the fixing plate 105, and the screw portions 106 a can be screwed into the screw holes 102 of the mounting portion 82.
  • the centering pin 104 has a cylindrical portion 104 a fitted in the through hole 101 of the mounting portion 82, a guide portion 104 b engaged with the engaging groove 103 of the fitting portion 83, and the mounting portion by the fixing bolt 106.
  • the fixing plate 105 fixed to 82 is in close contact with each other to prevent dropping.
  • the centering pin 104 is fixed to the combustor casing 41 side, and the guide portion 104 b is connected to the intermediate shaft cover 61 via the engagement groove 103.
  • the engagement groove 103 is provided along the radial direction of the combustor casing 41 and the intermediate shaft cover 61, the combustor casing 41 and the intermediate shaft cover 61 are centered with respect to the thermal extension. If it deviates, it can move relative.
  • FIG. 11 is a flowchart showing a work procedure of a combustor maintenance method
  • FIGS. 12 and 13 are schematic views showing a method of fixing the intermediate shaft cover by a fixing pad.
  • the gas turbine assembling method of the present embodiment includes a step of radially fitting the upper casing 42 of the combustor casing 41 to the end of the intermediate shaft cover 61 so as to cover the plurality of combustors 12, and a support pad 87.
  • the gas turbine maintenance method includes a step of releasing the fastening of the upper casing 42 in the combustor casing 41, a step of lifting the upper casing 42 from the lower casing 43 and releasing the upper casing 42, and the combustor 12.
  • Maintenance step a step of radially fitting the intermediate shaft cover 61 so as to cover the plurality of combustors 12 by the upper casing 42, and a fitting of the upper casing 42 and the intermediate shaft cover 61 by the support pad 87.
  • step 11 the nozzle portion in the combustor 12 is removed.
  • the nozzle portion includes a pilot combustion burner 54, a main combustion burner 55, a top hat portion 56, and fuel ports 57, 58 and 59.
  • step S12 the detent mechanism 73 is released.
  • the fixing bolt 93 is loosened, the nut 94 is loosened to remove the fixing plate 92, and the locking rod 91 is removed from the through hole 84.
  • the support pad 87 is released from the locking of the support pad 87 by removing the locking portion 91c of the locking rod 91 from the locking hole 87c.
  • the head of the fixing bolt 93 and the threaded portion 91a (the nut 94) of the locking rod 91 are cut by a cutting tool from the through hole 84.
  • the locking rod 91 can be extracted.
  • step S13 the centering pin 104 is removed.
  • the two fixing bolts 106 are loosened, the fixing plate 105 is removed from the mounting portion 82, a tool (not shown) is screwed into the screw hole 104d of the centering pin 104, and the centering is performed via the tool.
  • the pin 104 is extracted from the through hole 101 and the engagement groove 103.
  • step S14 the bolts 46 and 47 to which the combustor casing 41 (upper casing 42) is fixed are removed. As shown in FIG. 1, by loosening the bolt 46, the upper casing 42 and the compressor casing 21 are released from being fastened, and by loosening the bolt 47, the upper casing 42 and the turbine casing 26 are fastened. Is released.
  • the upper casing 42 is removed in step S15.
  • the jack 45 is disposed between the notch portion 42 b in the outer peripheral flange portion 42 a of the upper casing 42 and the outer peripheral flange portion 43 a in the lower casing 43. And by extending this jack 45, the upper casing 42 is lifted with respect to the lower casing 43, and both are separated.
  • the upper casing 42 is pressed and supported by the intermediate shaft cover 61 by the support pad 87, the upper casing 42 is separated from the lower casing 43 by applying a load larger than the pressing support force by the jack 45.
  • the support pad 87 is reversely rotated by the tool T, the support pad 87 is retracted along the axial direction of the screw hole 85, and the pressing portion 87b is recessed 86. Store it inside.
  • step S16 the maintenance work for the combustor 12 is performed in step S16.
  • the plurality of combustors 12 are exposed, so that an operator can perform maintenance work on the combustors 12.
  • the upper casing 42 is attached in step S17. As shown in FIGS. 2 and 12, the upper casing 42 is lowered and placed on the lower casing 43, and the fitted portion 81 is fitted to the fitting portion 83 of the intermediate shaft cover 61, and a plurality of bolts 44 is fastened.
  • step S ⁇ b> 18 the upper casing 42 is fixed by the bolts 46 and 47. As shown in FIG. 1, the upper casing 42 and the compressor casing 21 are fastened by fastening the bolt 46, and the upper casing 42 and the turbine casing 26 are fastened by fastening the bolt 47.
  • the centering pin 104 is attached in step S19.
  • the cylindrical portion 104 a of the centering pin 104 is fitted into the through hole 101 of the mounting portion 82, and the guide portion 104 b is engaged with the engaging groove 103 of the fitting portion 83.
  • the fixing plate 105 is brought into close contact with the mounting portion 82, and the fixing plate 105 is fixed by the fixing bolt 106.
  • the combustor casing 41 and the intermediate shaft cover 61 are supported by relative movement because their center positions are deviated from the thermal extension.
  • the support pad 87 is attached in step S20.
  • the locking portion T ⁇ b> 1 in the tool T is locked from the through hole 84 to the locking hole 87 c, and the support pad 87 is rotated forward by the tool T.
  • the support pad 87 advances along the axial direction of the screw hole 85, the pressing portion 87 b presses against the fitted portion 81 in the combustor casing 41, and the fitting portion 83 presses against the attachment portion 82. Therefore, the intermediate shaft cover 61 is pressed and supported by the combustor casing 41.
  • step S21 the detent mechanism 73 is mounted.
  • the locking portion 91 c of the locking rod 91 is locked from the through hole 84 to the locking hole 87 c of the support pad 87, and the flange portion 91 b is fitted into the through hole 84.
  • the fixing plate 92 is brought into close contact with the mounting portion 82 so that the screw portion 91a of the locking rod 91 passes through the first through hole 92a, and the fixing plate 92 is fixed to the mounting portion 82 with the fixing bolt 93, and the nut 94 Is fastened to the threaded portion 91 a of the locking rod 91. Therefore, when the locking rod 91 is fixed to the combustor casing 41, the rotation thereof is restricted, and the rotation of the support pad 87 on which the locking rod 91 is hooked is also restricted.
  • the nozzle part is mounted in step S22.
  • a pilot combustion burner 54, a main combustion burner 55, a top hat portion 56, and fuel ports 57, 58 and 59 are attached to the combustor 12.
  • the maintenance work of the combustor 12 is completed.
  • the rotating machine is configured by the combustor casing 41 including the upper and lower casings 42 and 43 having a half crack shape and the upper and lower casings 61 and 62 having a half crack shape.
  • Press support that presses and supports the intermediate shaft cover 61 that supports the combustor 12 in the combustor casing 41, the fitted portion 81 of the combustor casing 41, and the fitting portion 83 of the intermediate shaft cover 61 in the axial direction of the rotor 32.
  • a mechanism 71 is provided.
  • the combustor casing 41 and the intermediate shaft cover 61 are pressed and supported in the axial direction by the pressing support mechanism 71, there is no screw engaging portion between the combustor casing 41 and the intermediate shaft cover 61, and the screw Burning of the part can be avoided. Therefore, the upper casing 42 of the combustor casing 41 can be removed from the intermediate shaft cover 61 simply by releasing the pressing of the combustor casing 41 and the intermediate shaft cover 61 by the pressing support mechanism 71.
  • the upper casing 42 and the intermediate shaft can be applied to the upper casing 42 by applying a load to the outside in the radial direction.
  • the upper casing 42 can be removed by releasing the pressure with the cover 61. As a result, it is possible to easily remove the combustor casing 41 and improve the maintainability of the internal combustion chamber.
  • a support pad 87 that is screw-engaged with the fitting portion 83 of the intermediate shaft cover 61 and presses against the fitted portion 81 of the upper casing 42 is provided. Therefore, the upper pad 42 and the intermediate shaft cover 61 can be pressed and released by the support pad 87 only by rotating the support pad 87, and the workability of the assembling work and the dismantling work in the combustor casing 41 can be achieved. Can be improved.
  • the fitted portion 81 of the upper casing 42 has a concave shape
  • the fitting portion 83 of the intermediate shaft cover 61 has a convex shape
  • the support pad 87 is formed on the fitting portion 83 of the intermediate shaft cover 61.
  • the screw is engaged. Therefore, when the fitting portion 83 having the convex shape of the intermediate shaft cover 61 is fitted to the fitting portion 81 having the concave shape of the upper casing 42, it is supported by pressing the upper casing 42 only by rotating the support pad 87. Alternatively, pressing can be released, and workability can be improved.
  • a rotation prevention mechanism 73 that prevents the support pad 87 from rotating is provided. Therefore, after the support pad 87 is rotated and the upper casing 42 and the intermediate shaft cover 61 are pressed and supported, the rotation of the support pad 87 is prevented by the anti-rotation mechanism 73. Release of the pressing support of the cover 61 is suppressed, and reliability can be improved.
  • a locking rod 91 that locks to the base end portion of the support pad 87, a fixing plate 92 that fixes the locking rod 91 to the upper casing 42, and a fixing bolt 93 A nut 94 is provided. Therefore, after the support pad 87 is rotated and the upper casing 42 and the intermediate shaft cover 61 are pressed and supported, the locking rod 91 is locked to the base end portion of the support pad 87 and fixed to the upper casing 42. Therefore, the rotation of the support pad 87 can be easily prevented with a simple configuration, and when the fixing rod is seized, the locking rod 91 can be removed by cutting the fixing rod. Can be improved.
  • a centering mechanism 72 that supports the intermediate shaft cover 61 so as to be movable in the radial direction with respect to the combustor casing 41 is provided. Therefore, since the intermediate shaft cover 61 is movable in the radial direction with respect to the combustor casing 41 by the centering mechanism 72, even if the heat spread occurs in the combustor casing 41 and the intermediate shaft cover 61, the center of both of them. Therefore, the reliability of the apparatus can be improved.
  • the intermediate force can be removed by simply releasing the pressing of the upper casing 42 and the intermediate shaft cover 61 by the support pad 87.
  • the upper casing 42 can be removed from the shaft cover 61. Even if the pressing of the upper casing 42 and the intermediate shaft cover 61 by the support pad 87 cannot be released, the upper casing 42 and the intermediate shaft cover 61 are applied to the upper casing 42 by applying a load to the outside in the radial direction. And the upper casing 42 can be removed. As a result, it is possible to easily remove the upper casing 42 and improve the maintainability of the combustor 12.
  • the support pad 87 is screw-engaged with the fitting portion 83 of the intermediate shaft cover 61, and the intermediate shaft cover 61 is fitted to the fitted portion 81 of the upper casing 42.
  • the portion 83 is fitted, the upper casing 42 and the intermediate shaft cover 61 are pressed by rotating the support pad 87. Accordingly, by simply rotating the support pad 87, the upper casing 42 and the intermediate shaft cover 61 can be pressed and released by the support pad 87, and the workability of the assembling work and the dismantling work in the upper casing 42 can be improved. Can be improved.
  • the upper casing 42 and the intermediate shaft cover 61 are pressed and supported by the support pad 87, and then the support pad 87 is prevented from rotating with respect to the upper casing 42 and the intermediate shaft cover 61. Therefore, the release of the pressing support between the upper casing 42 and the intermediate shaft cover 61 due to vibration or the like is suppressed, and the reliability can be improved.
  • a step of releasing the fastening of the upper casing 42 in the combustor casing 41, a step of raising the upper casing 42 with respect to the lower casing 43 and releasing it The step of maintaining the combustor 12, the step of radially fitting the intermediate shaft cover 61 so as to cover the plurality of combustors 12 by the upper casing 42, and the upper casing 42 and the intermediate shaft cover 61 by the support pad 87 And a step of pressing and supporting the fitting portion in the axial direction of the rotor 32 and a step of fastening the upper casing 42.
  • the intermediate shaft can be simply released by releasing the pressing of the upper casing 42 and the intermediate shaft cover 61 by the support pad 87.
  • the upper casing 42 can be removed from the cover 61. Even if the pressing of the upper casing 42 and the intermediate shaft cover 61 by the support pad 87 cannot be released, the upper casing 42 can be removed by applying a load to the upper casing 42 radially outward. As a result, it is possible to easily remove the combustor casing 41 and improve the maintainability of the combustor 12.
  • the support pad 87 is provided as the pressing support mechanism 71.
  • the present invention is not limited to this configuration.
  • the screw portion 87a and the pressing portion 87b are integrally formed with the support pad 87, they may be configured to be integrally fixed as separate members.
  • the support pad 87 is provided on the intermediate shaft cover 61 side and is pressed against the combustor casing 41 side.
  • the support pad 87 is provided on the combustor casing 41 side and is pressed on the intermediate shaft cover 61 side. It may be configured.
  • the hexagonal locking hole 87c of the support pad 87 is formed as the anti-rotation mechanism 73, and the hexagonal locking portion 91c of the locking rod 91 is latched.
  • This shape is not limited to a hexagon, and may be another polygon, a cross, a plurality of holes (projections), or the like.
  • the fixing plate 92, the fixing bolt 93, and the nut 94 are provided as the fixing members.
  • the present invention is not limited to this configuration, and any configuration can be used as long as the locking member can be fixed in a non-rotatable manner. Good.
  • the combustor 12 supported by the intermediate shaft cover 61 is used as the structure supported by the inner casing, but is not limited to this relationship.
  • the rotary machine of this invention was demonstrated applying to a gas turbine, you may apply to a steam turbine as another rotary machine, for example.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PCT/JP2015/061163 2014-06-09 2015-04-09 回転機械及び回転機械の組立方法、回転機械のメンテナンス方法 WO2015190169A1 (ja)

Priority Applications (4)

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KR1020167032646A KR101874732B1 (ko) 2014-06-09 2015-04-09 회전 기계, 회전 기계의 조립 방법, 및 회전 기계의 메인터넌스 방법
US15/313,392 US10174676B2 (en) 2014-06-09 2015-04-09 Rotary machine, method of assembling rotary machine, and method of performing maintenance of rotary machine
DE112015002713.0T DE112015002713B4 (de) 2014-06-09 2015-04-09 Rotationsmaschine, Verfahren zum Zusammenbau einer Rotationsmaschine, und Verfahren zur Durchführung einer Wartung einer Rotationsmaschine
CN201580027305.4A CN106460561B (zh) 2014-06-09 2015-04-09 旋转机械以及旋转机械的组装方法、旋转机械的维护方法

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JP2014-118815 2014-06-09
JP2014118815A JP5869051B2 (ja) 2014-06-09 2014-06-09 回転機械及び回転機械の組立方法、回転機械のメンテナンス方法

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DE112015002713B4 (de) 2022-11-10
CN106460561B (zh) 2018-04-13
US20170184031A1 (en) 2017-06-29
JP5869051B2 (ja) 2016-02-24
DE112015002713T5 (de) 2017-03-02
KR101874732B1 (ko) 2018-07-04
CN106460561A (zh) 2017-02-22
US10174676B2 (en) 2019-01-08
JP2015232285A (ja) 2015-12-24
KR20160146920A (ko) 2016-12-21

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